Problem

Using the results of Section 5.4.1, repeat the task in Problem 2.11: Find an expression fo...

Using the results of Section 5.4.1, repeat the task in Problem 2.11: Find an expression for the maximum lift-to-drag ratio for a supersonic two-dimensional flat plate, and the angle of attack at which it occurs. Check your results with those from Problem 2.11. They should be identical.

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Solutions For Problems in Chapter 5